Boeing 737-301

Service difficulty reports · 4,797

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737301'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAA991200Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK BS 480 STRINGER 9R BELTFRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991199Angle · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706 AT STRINGER 11L ANGLE. REPLACED WITH IDENTICAL PART 6623574. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991165Stringer · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER 4 JUST AFT OF STATION 303.3. INSTALLED REPAIR ZEE AND FILLER PER SRM 53-00-03 AND EA 65951. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA991164Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER DOOR FRAME SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-01 FIG 202. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991150Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO .75 INCH AREAS OF CORROSION AT STATION 328, BL 0, AND LBL 28 FLOORBEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. INSTALLED T-CAP AND DOUBLER PER SRM 53-10-51. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991149Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 480 STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991148Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 616 STRINGER 2R TIE CLIP. REPLACED PER SRM 51-40-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991147Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 887 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991146Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACK AT BS 827 STRINGER 9L BELT FRAME. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991145Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 827 STRINGER 9R BELT FRAME. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER EA 65850. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, FrameSDR USAA991144Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178 BULKHEAD RBL .5, WL 188 WEB. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER PER SRM 53-10-08. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991143Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 178 BULKHEAD LBL. 5, WL 188 WEB. CUTOUT DAMAGE AREA AND INSTALLED DOUBLER PER SRM 53-10-08. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991142Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 178 RBL 4.75, WL 198 SKIN. INSTALLED FILLERS AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991141Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FUOND A .75 INCH CRACK AT STATION 178 LBL 4.78, WL 198 SKIN. INSTALLED FILLERS AND DOUBLERS PER SRM 51-10-02 AND TR 53-10-07. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991140Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT STATION 178 LBL 4.75, WL 201 SKIN. INSTALLED FILLERS AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991139Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 178 BULKHEAD RBL 4.75, WL 201 SKIN. INSTALLED FILLERS AND DOUBLER PER SRM 51-10-02 AND TR 53-10-07. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA991138Splice · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .01 INCH CRACK AROUND TWO RIVETS AT STATION 908 AND STRINGER 4L STRINGER SPLICE. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991137Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT ACCESS PANEL OUTBOARD EDGE CUTOUT PYLON SKIN. INSTALLED DOUBLER PER TR 54-30-07. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA991136Splice · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .01 INCH CRACK STATION 908, STRINGER 4R IN STRINGER SPLICE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991135Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK BETWEEN STRINGERS 10 AND 11 AND STATION 291.5 SHEAR TIE. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991134Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGERS 12 AND 13 AND BETWEEN STATION 291.5 AND 277 SHEAR TIE. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991133Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STRINGER NR 14 STATION 277 SHEAR TY WEB. REMOVED AND REPLACED WEB PER ARM 51-40-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991132Support · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STRINGER SUPPORT BETWEEN STATION 303.3 - 294.5 HORIZONTAL SUPPORT. INSTALLED NEW FABRICATED SUPPORT PER SRM 51-10-2. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991131Shear Tie · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BETWEEN STRINGER 11 AND 12 AND STATION 291.5 AND 277 SHEAR TIE. REPLACED WITH IDENTICAL PART PER SRM 51-40-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991101Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND 7.25 INCH AT FLOORBOARD FASTENERS HOLES FLOORBEAM 312 LBL 11 TO RBL 11. CORROSION LEVEL 2. INSTALLED 'T' CAP AND DOUBLER EPR SRM 53-10-51. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991100Angle · corrodedCLT - DURIGN Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 2 INCH BY 32 INCH AT LBL 55 STATION 312 TO 344 FLOORBEAM LEFT Z ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-01. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991094Angle · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORRODED AREA AFT SERVICE DOOR Z-ANGLE STATION 967 TO 986.5, WL 208. CORROSION LEVEL 1. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991093Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 344 FLOORBEAM UPPER FLANGE LBL 12 TO RBL 10. CORROSION LEVEL 1. NEW SECTION SPLICED IN PER SRM 53-10-51. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991084Floorbeam · corrosionCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 8 INCH AT FLOORBEAM BS 986.5, LBL 44 TO RBL 44 BEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. REPLACED CORRODED AREA PER SRM 53-00-51. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991082Angle · crackedCLT - DURING Q-1/CX-6 CHECK VISUAL INSPECTION, FUOND A .25 INCH CRACK AT STATION 706, STRINGER 11L AFT SIDE OF FRAME ATTACH ANGLE. FABRICATED NEW ANGLE PER DRAWING 66-23574. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991044Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CRACK .25 INCH AT STATION 663 STRINGER 10R TIE CLIP. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991043Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 CRACKS EACH .25 INCH AT STATION 663 STRINGER 10L. REPLACED WITH IDENTICAL PART PER SRM 53-10-2. (M)Oct 29, 1999 · N559AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB99259Windshield · crackedCLT - FLT 1217 - EN ROUTE FROM PIT TO DFW, AT FL350, CREW HEARD A LOUD POPPING NOISE. CAPTAIN NOTICED THE FIRST OFFICERS NR 1 WINDSHIELD HAD MULTIPLE CRACKS AND WAS ARCING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAREOct 26, 1999 · N336US · Boeing 737301 · Flight Compartment WindowsSDR USAASB99258Indicator · malfunctionedBWI - FLT 2438 - AFTER TAKEOFF, THE FLAPS WOULD NOT RETRACT FROM THE FIVE DEGREE POSITION. FLAP HANDLE WOULD NOT MOVE FLAPS UP OR DOWN. FLIGHT DIVERTED TO BWI AND AN EMERGENCY WAS DECLARED. ALTERNATE FLAP EXTENSION WAS USED TO POSITION FLAPS TO 15 DEGREES FOct 24, 1999 · N352US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAASB99252Selector Panel · failedCLT - FLT 858 - ON CLIMB-OUT FROM CLT, THE AIRCRAFT WOULD NOT PRESSURIZE. CAPTAIN COULD NOT CONTROL PRESSURIZATION IN AUTO, STANDBY OR MANUAL MODE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE Oct 18, 1999 · N585US · Boeing 737301 · Cabin Pressure Control SystemSDR USAA991130Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AT STATION 867, RBL 13.80 FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. REMOVED CORROSION PER SRM 53-00-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991129Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 2 INCH AT STATION 847 BETWEEN STRINGER 24R AND 25R FRAME. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. INSTALLED DOUBLER AND FILLER PER SRM 53-00-07 FIG 201 AND EA 65717. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991128Pan · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA 1 INCH BY 1 INCH AND A 2 INCH BY 2 INCH AT FORWARD AND AFT ENDS STATION 807 AND 847, RBBL 20 AFT CARGO DOOR THRESHOLD PAN. CORROSION LEVEL 1. CORROSION TASK NR C53-208-01. REMOVED AND REPLACED Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991092Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 540, STRINGER 22R SUPPORT ANGLE RAM AIR INLET SUPPORT. FABRICATED AND INSTALLED REPLACEMENT REPAIR ANGLE PER 53-50-03. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991091Skin · crackCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK LOWER AFT CORNER OF PANEL NR 5727L CUTOUT LEFT PYLON SKIN. INSTALLED DOUBLER PER EA 65815 AND TR 54-30-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA991080Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 1016, RBL 6, RBL 27, RBL 29 LWR SURFACE OF T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991079Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT BS 1006, LBL 38 T-CAP BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. REMOVED AND REPLACED BEAM PER TR 53-10-05. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991078Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AND 1 INCH UPPER CHORD STATION 328, LBL 28 BEAM. CORROSION LEVEL 1. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991077Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 379, LBS 3.5 SKIN. INSTALLED REPAIR DOUBLER PER TR-53-30-07 AND BAC DRWG 65C33930. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991076Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .0125 INCH CRACK AT BS 827 STRINGER 9R AT FASTENER HOLE FRAME. INSTALLED DOUBLER PER EA 65542, SRM 53-00-07 AND SRM 53-30-07. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991075Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT FORWARD SERVICE DOOR CUTOUT FRAME STATION 295.5, RBL 54, WL 208.5. FABRICATED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, FrameSDR USAA991074Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 CRACKS, 1 AT 1.25 INCH LONG AND 1 AT .0675 INCH LONG EMANATING FROM RIVETS IN FUS AT LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED DOUBLER PER SRM 53-10-01. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991071Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .250 INCH BY .250 INCH AREA OF CORROSION AT BS 344, LBL 51, RBL 15 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-01. INSTALLED T-CAP PER EA 65749 AND SRM 53-10-51. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991059Shear Beam · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT STATION 726, STRINGER 18A RIGHT, RBL 61, WL 188 SHEAR BEAM WEB. INSTALLED NEW WEB AND GUSSETT PLATE PER EA 65576 AND SB 737-53-1170. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991056Channel · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT STATION 359 STRINGER 14L IN TIE CHANNEL TO STRINGER. INSTALLED NEW CHANNEL PER EA 65686. (M)Oct 18, 1999 · N340US · Boeing 737301 · Fuselage Miscellaneous Structure
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